US20060070689A1 - Method of heat treating an aluminium alloy member and apparatus therefor - Google Patents

Method of heat treating an aluminium alloy member and apparatus therefor Download PDF

Info

Publication number
US20060070689A1
US20060070689A1 US11/239,477 US23947705A US2006070689A1 US 20060070689 A1 US20060070689 A1 US 20060070689A1 US 23947705 A US23947705 A US 23947705A US 2006070689 A1 US2006070689 A1 US 2006070689A1
Authority
US
United States
Prior art keywords
aluminium alloy
ageing
heat treatment
heating plate
alloy member
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
US11/239,477
Other versions
US7491278B2 (en
Inventor
Ingo Kropfl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Novelis Koblenz GmbH
Original Assignee
Corus Aluminium Walzprodukte GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Corus Aluminium Walzprodukte GmbH filed Critical Corus Aluminium Walzprodukte GmbH
Priority to US11/239,477 priority Critical patent/US7491278B2/en
Assigned to CORUS ALUMINIUM WALZPRODUKTE GMBH reassignment CORUS ALUMINIUM WALZPRODUKTE GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KROPFL, INGO GUNTHER
Publication of US20060070689A1 publication Critical patent/US20060070689A1/en
Assigned to ALERIS ALUMINUM KOBLENZ GMBH reassignment ALERIS ALUMINUM KOBLENZ GMBH CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: CORUS ALUMINIUM WALZPRODUKTE GMBH
Application granted granted Critical
Publication of US7491278B2 publication Critical patent/US7491278B2/en
Expired - Fee Related legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon

Definitions

  • This invention relates to a method of heat treating an aluminium alloy member, comprising a pre-ageing heat treatment step, and an apparatus therefor.
  • Aluminium alloy members made of heat-treatable aluminium alloys are used in a number of applications involving relatively high strength, high toughness and corrosion resistance such as aircraft fuselages, vehicular members and other applications.
  • aluminium alloy is either direct chill cast as ingots or continuous cast in the form of a thick strip material, and then hot rolled and/or cold rolled to the desired thickness.
  • the member then undergoes solution heat treatment.
  • Solution heat treatment involves heating the metal to a suitably high temperature (e.g. 450-580° C.) to cause dissolution into solid solution of all the soluble alloying constituents that precipitated from the parent metal during hot and/or cold rolling. To retain these constituents in solid solution, the metal is rapidly quenched to ambient temperature to create a solid supersaturated solution.
  • the metal is then aged or precipitation hardened by holding the metal at room temperature, or at a higher temperature to accelerate the effect, for a period of time to cause the spontaneous formation of fine precipitates through the diffusion of atoms in the supersaturated solid solution, whereby they form fine clusters or “zones”.
  • an aluminium alloy member may be further improved by subjecting the member to a further heat treatment after quenching.
  • pre-ageing so called “pre-ageing” heat treatment, some of the atoms in the supersaturated solid solution come out of the lattice structure and form seeds for the formation of fine clusters. This serves to stabilize the microstructure.
  • U.S. Pat. No. 3,135,633 discloses such a pre-ageing or “stabilizing” heat treatment to improve the mechanical properties of aluminium-magnesium-silicon alloys.
  • wrought alloyed products are moved continuously through a first furnace to put the relevant alloying elements into solid solution, then through a quenching chamber and into a second furnace to be subjected to a stabilizing pre-ageing treatment. It is mentioned that the time interval between quenching and preliminary ageing should be less than ten minutes. To allow for rapid heating-up of the alloy, starting a few minutes after quenching, the second furnace is heated by forced hot air circulation.
  • a pre-ageing heat treatment is further described in EP-0805879-B1.
  • the metal is heated directly to a peak temperature in the range of 100 to 300° C., preferably in the range of 130 to 270° C., is maintained at the peak temperature for a very short dwell time and is then cooled directly to below a defined final temperature.
  • This treatment is therefore also referred to in the art as temperature “spiking”, since the profile of the temperature versus time graph for such a process resembles a generally triangular, pointed, or slightly blunted spike.
  • the treatment is reported to improve the ductility of alloys of a AA6xxx-series in the T4 temper while maximizing the paint bake response.
  • EP-0480402-A1 Another process involving a pre-ageing heat treatment is disclosed in EP-0480402-A1.
  • the known process involves quenching an aluminium alloy sheet after solution heat treatment, allowing the sheet to hold still at room temperature for less than 60 minutes, and holding the sheet at a temperature of 50-150° C. for a period of from 10-500 minutes.
  • EP-0679199-A1 also discloses a pre-ageing or pre-tempering step at a temperature of 70 to 150° C. in between the quenching after solution heat treatment and ageing steps.
  • the present invention solves preferably one or more of the above-mentioned objects. Preferred embodiments are described and specified by this specification.
  • the present invention relates to a method of heat treating an aluminium alloy member having a main surface, including the steps of (a) subjecting the member to a solution heat treatment (b) quenching the member and (c) reheating the member in a pre-ageing heat treatment step.
  • the pre-ageing heat treatment is conducted by holding the aluminium alloy member close to a heating plate.
  • the invention is also directed to a product produced according to this method, and to an apparatus for performing the pre-ageing heat treatment.
  • alloy designations and temper designations refer to the Aluminum Association designations in Aluminum Standards and Data and the Registration Records, as published by the Aluminum Association.
  • a method of heat treating an aluminium alloy member having a main surface comprising the steps in succession of a) subjecting the member to a solution heat treatment, b) quenching the member, preferably by one of spray quenching or immersion quenching in water or other quenching media, and c) reheating the quenched member in a pre-ageing heat treatment step, and whereby the pre-ageing heat treatment is conducted by coupling the main surface of the aluminium alloy member to a main surface of a heating plate.
  • the invention is based on the realisation that the pre-ageing heat treatment is particularly effective when if it is performed directly after the quenching step of the member terminating the solution heat treatment to obtain a more stabilised microstructure of the aluminium alloy member without substantial natural age hardening taking place. More preferably, the pre-ageing treatment is carried out within one hour of the quenching step and the time delay is usually reduced to a matter of minutes and possibly even to seconds. For this reason, conducting the heat treatment in a furnace will not yield ideal results, because the member has to be moved into the furnace, and will take some time to reach the desired temperature.
  • the invention therefore proposes a method without utilising a furnace for the pre-age treatment of the aluminium alloy member as the pre-aging treatment is carried out outside any furnace.
  • the aluminium alloy member is held close to or coupled to a heating plate and is thereby rapidly heated up to achieve a pre-ageing treatment.
  • the maximum pre-ageing temperature may be reached within a few minutes, since heat is transferred from the heating plate to the aluminium alloy member.
  • the heating plate is preferably already heated up to the desired temperature prior to the pre-ageing step.
  • the aluminium alloy member on which this method is performed is preferably a rolled product, typically a thin plate or a sheet having a thickness of at most 15 mm and preferably in the range of 1.5 to 6 mm.
  • the method may be used for the treatment of any heat-treatable aluminium alloy, in particular those of the AA6xxx, AA2xxx, or AA7xxx-series aluminium alloys.
  • the aluminium alloy member is selected from the group consisting of AA6013, AA6056, M6011, AA6016, A2024, AA2524, M2219, M7074, AA7075, M7050 and M7055.
  • the heating plate is preferably also made of an aluminium alloy having a large heat capacity and a higher melting point relative to the heat treated aluminium alloy member.
  • aluminium alloys of the AA5xxx-series such as for example AA5026, and the M3xxx-series can be used.
  • the thickness of the heating plate is at least the thickness of the thickness of the aluminium alloy member. The skilled person will be able to optimize the thickness of the heating plate depending of the thickness of the aluminium alloy member and the desired pre-ageing treatment temperature and time.
  • the heating plate is made from a steel.
  • the heating plate is being placed in the furnace used for the solution heat treatment together with the aluminium alloy member.
  • This method has the advantage that no extra equipment or time is needed to heat up the heating plate.
  • the aluminium alloy member and the heating plate are both held substantially horizontal, and the aluminium alloy member is simply placed on top of the heating plate before entering the furnace used for solution heat treatment.
  • the heating plate and the member are held with their main surfaces close to each other during all three steps of solution heat treatment, quenching and pre-ageing.
  • the member may be quenched by spraying or cooling from one side only.
  • this has the advantage that the member will be re-heated to achieve a pre-ageing treatment immediately after quenching has been finished by a heat flow from the non-quenched heating plate to the aluminium alloy member.
  • the aluminium plate is quenched on both sides and it is placed on the heating plate to achieve the desired pre-ageing treatment.
  • the heating plate may be placed in the furnace used for the solution heat treatment before the aluminium alloy member is solution heat treated. Once it has been heated up, the heating plate may be kept near the quenching apparatus during the solution heat treatment and quenching of the aluminium alloy member. Since the maximum temperature of the pre-ageing treatment is typically lower than the temperature of the solution heat treatment, it may even be advantageous to let the heating plate cool down before it receives the aluminium alloy member. After quenching, the aluminium alloy member is preferably lifted on top of the heating plate.
  • a further alternative concerns heating the heating plate electrically, for example by means of heating coils disposed inside the heating plate.
  • a protective layer is placed between each aluminium alloy member and each heating plate to couple them together.
  • This layer has a thickness preferably up to 5 mm, and typically a thickness of about 2 mm, and is made from a cloth or web made of an isolating material such as glass fabric, ceramics, glass wool, mineral wool or, for lower temperatures, a polymer fabric.
  • the use of the protective layer will also result into a small delay of the reheating of the aluminium alloy member resulting that in the quenching operation the member is allowed to cool down fast to below 100° C. prior to receiving the heat from the heating plate to achieve a pre-ageing heat treatment.
  • the aluminium alloy member is held sandwiched between two heating plates during the pre-ageing step. This arrangement serves to straighten the member, so that no further levelling or stretching operation may be required.
  • two aluminium alloy members are being heat treated at the same time by being held close to opposite sides of one heating plate.
  • the pre-ageing treatment according to the invention is carried out prior to bringing the aluminium alloy member to its final temper by means of artificial ageing.
  • Typical final temper would be a temper selected from the group comprising T6, T79, T78, T77, T74, T73 and T8.
  • a suitable T73 temper would be a T7351 temper
  • a suitable T74 temper would be the T7451 temper.
  • the aluminium alloy member may optionally be stretched or compressed or otherwise cold worked to relieve stresses or to improve mechanical properties, for example levelling of the sheet or thin plate products.
  • the stretching operation involves not more than 8% of the length just prior to the stretching operation, and is preferably in a range of 1 to 5%.
  • aluminium alloy members of the AA6xxx-and AA2xxx-series alloys can be subjected also to a cold rolling operation with a cold rolling reduction in a range of up to 20% to improve achievable mechanical properties in the final temper.
  • the invention relates to a product obtained by the method according to this invention.
  • the final product may for example be used for the outer skin of aircraft fuselages.
  • the invention in another aspect provides an apparatus for heat treating an aluminium alloy member comprising: a) a solution heat treatment furnace, b) a quenching station, c) a heating plate for reheating the member in a pre-ageing heat treatment step by coupling a main surface of the member to a main surface of the heating plate.
  • This apparatus has the advantage that it does not require a second furnace for the pre-ageing heat treatment.
  • FIG. 1 is a schematic representation of a heat treatment facility according to the prior art
  • FIG. 2 is a schematic representation of a heat treatment facility using a method according to a first embodiment of the invention
  • FIG. 3 is a temperature versus time graph for the method according to the first embodiment
  • FIG. 4 is a cross sectional view of an arrangement of aluminium alloy member and heating plate according to the first embodiment
  • FIG. 5 is a cross sectional view of an arrangement of two members and the heating plate according to a second embodiment
  • FIG. 6 is a schematic representation of a heat treatment facility using a method according to a third embodiment of the invention
  • FIG. 7 is a cross sectional view of member/heating plate arrangement according to a further embodiment.
  • FIG. 1 shows a state of the art facility for heat treating an aluminium alloy member 1 .
  • the member 1 coming from the rolling mill is solution heat treated in a continuous horizontal furnace 4 .
  • the member 1 is conveyed through the furnace on rollers 6 .
  • the member 1 is quenched by means of nozzles 8 a, 8 b, which spray quenching water onto be upper and lower surfaces of the member.
  • a further horizontal furnace 10 is provided at the end of the line.
  • the pre-ageing furnace 10 must be specially equipped with forced hot air circulation to ensure rapid reheating of the member 1 .
  • FIG. 2 A facility implementing the method according to the first embodiment of the invention is shown in FIG. 2 .
  • the plate 1 coming from the mill is again heat treated in a horizontal furnace 4 . However, it is disposed on top of a heating plate 12 during the treatment. After the solution heat treatment, the member 1 remains on the heating plate while undergoing quenching. Hence, only the upper nozzles 8 a are used to quench member 1 .
  • the member/plate arrangement is then further conveyed on rollers 6 . Since plate 12 is as thick as or thicker than member 1 and made of a material of high heat capacity and good heat conductivity, plate 12 will reheat the member 1 immediately after quenching has stopped.
  • the heating rate and the maximum temperature reached by the member will depend on the thickness and composition of the heating plate 12 in relation to the thickness and composition of the member 1 .
  • the heating plate is about 40 mm thick, i.e. thicker than the member 1 , and is preferably made of an aluminium alloy of the AA5xxx-series or AA3xxx-series.
  • the temperature profile experience by the member 1 is shown in FIG. 3 .
  • the member 1 is heated to a first temperature T 1 , which is between 450° C. and 580° C., and typically about 530° C.
  • the metal is held at this temperature for some time as known in the art.
  • the metal is rapidly cooled down to a temperature of 100° C. or less, preferably to room temperature RT.
  • T 2 a pre-ageing temperature
  • the member will reach T 2 within a few minutes and will preferably be held at this temperature for a time required to achieve the desired pre-ageing effect, and the holding time would typically be in the range of up the 30 minutes, preferably 10 to 20 minutes.
  • the selected pre-ageing temperature and holding time will be dependent on the alloy composition of the aluminium alloy member.
  • the pre-ageing treatment is finalised by taking off the aluminium alloy member from the heating plate. The member is then cooled down to ambient temperature by means of water cooling, forced air or left on for example a roller table to cool down by free air convention. The cooling rate after the pre-ageing treatment has been found not to be very critical.
  • reheating to achieve the pre-ageing effect will begin within one or two minutes, preferably within 0 to 20 seconds, after quenching from solution heat treatment.
  • the heating rate is preferably in the range of 10 to 50° C./min., so that the final pre-ageing temperature will be reached within 1 to 10 minutes, preferably 5 minutes.
  • FIG. 4 shows an enlarged cross sectional view of the member/plate arrangement.
  • a protective layer 14 to space the member 1 and the plate 12 from each other, and to provide a heat isolating layer between the member 1 and the plate 12 .
  • the protective layer 14 is about 2 mm thick and made of a heat isolating fabric such as glass fabric, glass wool, mineral wool or polymer fabric.
  • a protective layer may be present in each case between each member 1 and each heating plate 12 .
  • one heating plate 12 will be sandwiched between two aluminium alloy members 1 , 1 ′ as shown in FIG. 5 .
  • the arrangement according to FIG. 5 allows the pre-ageing treatment of two members 1 , 1 ′ simultaneously.
  • the heating plate 12 must be thick enough to store sufficient heat for re-heating both members to achieve the required pre-ageing treatment.
  • These first two embodiments are suitable for continuous heat treatment, in which the heating plate(s) and the aluminium alloy member(s) are held adjacent to each other during all steps of solution heat treatment, quenching and pre-ageing.
  • FIG. 6 it may be advantageous in some applications to heat up the heating plate 12 before the aluminium alloy member 1 .
  • This arrangement is shown in FIG. 6 .
  • the plate 12 will be heated before the solution heat treatment of member 1 in the horizontal furnace 4 and then placed aside. After quenching, the member 1 will be lifted on top of the heating plate 12 .
  • This embodiment has the advantage that the plate 12 may have cooled down to the lower pre-ageing temperature in the range of 100 to 250° C. before receiving the member 1 .
  • the member 1 may be fed through the solution heat treatment furnace before the heating plate 12 .
  • the embodiment shown in FIG. 6 also allows to use a self-heating plate 12 provided e.g. with electrical coils, which need not be heated up in a furnace.
  • two heating plates 12 , 12 ′ will be heated prior to the pre-ageing step, and one heating plate 12 ′ will be placed on top of member 1 . This will straighten the member 1 , so that further stretch forming may not be necessary.
  • the member After the member has cooled down to ambient temperature the member will undergo a further ageing treatment to produce an age-hardened material with the desired set of properties for its application.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatments In General, Especially Conveying And Cooling (AREA)

Abstract

Disclosed is a method of heat treating an aluminium alloy member having a main surface, including the steps of (a) subjecting the member to a solution heat treatment (b) quenching the member and (c) reheating the member in a pre-ageing heat treatment step. The pre-ageing heat treatment is conducted by holding the aluminium alloy member close to a heating plate. Also disclosed is a product produced according to this method, and to an apparatus for performing the pre-ageing heat treatment.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This claims priority from U.S. provisional patent application No. 60/616,228 filed Oct. 7, 2004 and European patent application no. 04077719.5 filed Oct. 5, 2004, both incorporated herein by reference in their entirety.
  • FIELD OF THE INVENTION
  • This invention relates to a method of heat treating an aluminium alloy member, comprising a pre-ageing heat treatment step, and an apparatus therefor.
  • BACKGROUND OF THE INVENTION
  • Aluminium alloy members made of heat-treatable aluminium alloys are used in a number of applications involving relatively high strength, high toughness and corrosion resistance such as aircraft fuselages, vehicular members and other applications.
  • To manufacture an aluminium alloy member, for example a sheet or plate, aluminium alloy is either direct chill cast as ingots or continuous cast in the form of a thick strip material, and then hot rolled and/or cold rolled to the desired thickness. The member then undergoes solution heat treatment. Solution heat treatment involves heating the metal to a suitably high temperature (e.g. 450-580° C.) to cause dissolution into solid solution of all the soluble alloying constituents that precipitated from the parent metal during hot and/or cold rolling. To retain these constituents in solid solution, the metal is rapidly quenched to ambient temperature to create a solid supersaturated solution. Usually, the metal is then aged or precipitation hardened by holding the metal at room temperature, or at a higher temperature to accelerate the effect, for a period of time to cause the spontaneous formation of fine precipitates through the diffusion of atoms in the supersaturated solid solution, whereby they form fine clusters or “zones”.
  • It is further known that the properties of an aluminium alloy member may be further improved by subjecting the member to a further heat treatment after quenching. During this so called “pre-ageing” heat treatment, some of the atoms in the supersaturated solid solution come out of the lattice structure and form seeds for the formation of fine clusters. This serves to stabilize the microstructure.
  • U.S. Pat. No. 3,135,633 discloses such a pre-ageing or “stabilizing” heat treatment to improve the mechanical properties of aluminium-magnesium-silicon alloys. In this process, wrought alloyed products are moved continuously through a first furnace to put the relevant alloying elements into solid solution, then through a quenching chamber and into a second furnace to be subjected to a stabilizing pre-ageing treatment. It is mentioned that the time interval between quenching and preliminary ageing should be less than ten minutes. To allow for rapid heating-up of the alloy, starting a few minutes after quenching, the second furnace is heated by forced hot air circulation.
  • A pre-ageing heat treatment is further described in EP-0805879-B1. In the disclosed method the metal is heated directly to a peak temperature in the range of 100 to 300° C., preferably in the range of 130 to 270° C., is maintained at the peak temperature for a very short dwell time and is then cooled directly to below a defined final temperature. This treatment is therefore also referred to in the art as temperature “spiking”, since the profile of the temperature versus time graph for such a process resembles a generally triangular, pointed, or slightly blunted spike. The treatment is reported to improve the ductility of alloys of a AA6xxx-series in the T4 temper while maximizing the paint bake response.
  • Another process involving a pre-ageing heat treatment is disclosed in EP-0480402-A1. The known process involves quenching an aluminium alloy sheet after solution heat treatment, allowing the sheet to hold still at room temperature for less than 60 minutes, and holding the sheet at a temperature of 50-150° C. for a period of from 10-500 minutes.
  • EP-0679199-A1 also discloses a pre-ageing or pre-tempering step at a temperature of 70 to 150° C. in between the quenching after solution heat treatment and ageing steps.
  • SUMMARY OF THE INVENTION
  • It is a preferred object of the present invention to further improve heat treatment methods for aluminium alloy members in order to further the properties of the final product.
  • It is a further object to simplify the apparatus required to carry out the the heat treatment, in particular the pre-ageing treatment after solution heat treatment.
  • The present invention solves preferably one or more of the above-mentioned objects. Preferred embodiments are described and specified by this specification.
  • The present invention relates to a method of heat treating an aluminium alloy member having a main surface, including the steps of (a) subjecting the member to a solution heat treatment (b) quenching the member and (c) reheating the member in a pre-ageing heat treatment step. The pre-ageing heat treatment is conducted by holding the aluminium alloy member close to a heating plate. The invention is also directed to a product produced according to this method, and to an apparatus for performing the pre-ageing heat treatment.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
  • As will be appreciated herein below, except as otherwise indicated, all alloy designations and temper designations refer to the Aluminum Association designations in Aluminum Standards and Data and the Registration Records, as published by the Aluminum Association.
  • According to one aspect of the invention there is provided a method of heat treating an aluminium alloy member having a main surface, the method comprising the steps in succession of a) subjecting the member to a solution heat treatment, b) quenching the member, preferably by one of spray quenching or immersion quenching in water or other quenching media, and c) reheating the quenched member in a pre-ageing heat treatment step, and whereby the pre-ageing heat treatment is conducted by coupling the main surface of the aluminium alloy member to a main surface of a heating plate.
  • The invention is based on the realisation that the pre-ageing heat treatment is particularly effective when if it is performed directly after the quenching step of the member terminating the solution heat treatment to obtain a more stabilised microstructure of the aluminium alloy member without substantial natural age hardening taking place. More preferably, the pre-ageing treatment is carried out within one hour of the quenching step and the time delay is usually reduced to a matter of minutes and possibly even to seconds. For this reason, conducting the heat treatment in a furnace will not yield ideal results, because the member has to be moved into the furnace, and will take some time to reach the desired temperature. The invention therefore proposes a method without utilising a furnace for the pre-age treatment of the aluminium alloy member as the pre-aging treatment is carried out outside any furnace. Instead of a furnace, the aluminium alloy member is held close to or coupled to a heating plate and is thereby rapidly heated up to achieve a pre-ageing treatment. The maximum pre-ageing temperature may be reached within a few minutes, since heat is transferred from the heating plate to the aluminium alloy member. The heating plate is preferably already heated up to the desired temperature prior to the pre-ageing step.
  • The aluminium alloy member on which this method is performed is preferably a rolled product, typically a thin plate or a sheet having a thickness of at most 15 mm and preferably in the range of 1.5 to 6 mm.
  • The method may be used for the treatment of any heat-treatable aluminium alloy, in particular those of the AA6xxx, AA2xxx, or AA7xxx-series aluminium alloys. Most preferred, the aluminium alloy member is selected from the group consisting of AA6013, AA6056, M6011, AA6016, A2024, AA2524, M2219, M7074, AA7075, M7050 and M7055.
  • The heating plate is preferably also made of an aluminium alloy having a large heat capacity and a higher melting point relative to the heat treated aluminium alloy member. In particular aluminium alloys of the AA5xxx-series, such as for example AA5026, and the M3xxx-series can be used. In this embodiment the thickness of the heating plate is at least the thickness of the thickness of the aluminium alloy member. The skilled person will be able to optimize the thickness of the heating plate depending of the thickness of the aluminium alloy member and the desired pre-ageing treatment temperature and time.
  • In another embodiment the heating plate is made from a steel.
  • There are several ways of heating up the heating plate prior to the pre-ageing step. In an embodiment, the heating plate is being placed in the furnace used for the solution heat treatment together with the aluminium alloy member. This method has the advantage that no extra equipment or time is needed to heat up the heating plate. Preferably, the aluminium alloy member and the heating plate are both held substantially horizontal, and the aluminium alloy member is simply placed on top of the heating plate before entering the furnace used for solution heat treatment.
  • Preferably, the heating plate and the member are held with their main surfaces close to each other during all three steps of solution heat treatment, quenching and pre-ageing. This means that the member may be quenched by spraying or cooling from one side only. However, this has the advantage that the member will be re-heated to achieve a pre-ageing treatment immediately after quenching has been finished by a heat flow from the non-quenched heating plate to the aluminium alloy member.
  • Alternatively, the aluminium plate is quenched on both sides and it is placed on the heating plate to achieve the desired pre-ageing treatment.
  • Alternatively, the heating plate may be placed in the furnace used for the solution heat treatment before the aluminium alloy member is solution heat treated. Once it has been heated up, the heating plate may be kept near the quenching apparatus during the solution heat treatment and quenching of the aluminium alloy member. Since the maximum temperature of the pre-ageing treatment is typically lower than the temperature of the solution heat treatment, it may even be advantageous to let the heating plate cool down before it receives the aluminium alloy member. After quenching, the aluminium alloy member is preferably lifted on top of the heating plate.
  • A further alternative concerns heating the heating plate electrically, for example by means of heating coils disposed inside the heating plate. In this embodiment, it is preferred to heat up the plate to the desired pre-ageing temperature before the pre-ageing heat treatment is conducted.
  • The usual way to hold the main surface of the aluminium alloy member close to a main surface of the heating plate will be to place them horizontally one on top of the other. However, arrangements in which the member and plate are vertically aligned are not excluded from the scope of protection.
  • In order to protect the surface of the aluminium alloy member and to ensure a small gap between the heated plate and the aluminium alloy member, a protective layer is placed between each aluminium alloy member and each heating plate to couple them together. This layer has a thickness preferably up to 5 mm, and typically a thickness of about 2 mm, and is made from a cloth or web made of an isolating material such as glass fabric, ceramics, glass wool, mineral wool or, for lower temperatures, a polymer fabric. The use of the protective layer will also result into a small delay of the reheating of the aluminium alloy member resulting that in the quenching operation the member is allowed to cool down fast to below 100° C. prior to receiving the heat from the heating plate to achieve a pre-ageing heat treatment.
  • It is also possible to use more than one heating plate. In a preferred embodiment, the aluminium alloy member is held sandwiched between two heating plates during the pre-ageing step. This arrangement serves to straighten the member, so that no further levelling or stretching operation may be required.
  • According to an alternative embodiment, two aluminium alloy members are being heat treated at the same time by being held close to opposite sides of one heating plate.
  • The pre-ageing treatment according to the invention is carried out prior to bringing the aluminium alloy member to its final temper by means of artificial ageing. Typical final temper would be a temper selected from the group comprising T6, T79, T78, T77, T74, T73 and T8. By means of example, a suitable T73 temper would be a T7351 temper, and a suitable T74 temper would be the T7451 temper.
  • In an embodiment after the pre-ageing treatment and prior to the final ageing treatment the aluminium alloy member may optionally be stretched or compressed or otherwise cold worked to relieve stresses or to improve mechanical properties, for example levelling of the sheet or thin plate products. Preferably the stretching operation involves not more than 8% of the length just prior to the stretching operation, and is preferably in a range of 1 to 5%. In particular aluminium alloy members of the AA6xxx-and AA2xxx-series alloys can be subjected also to a cold rolling operation with a cold rolling reduction in a range of up to 20% to improve achievable mechanical properties in the final temper.
  • In another aspect the invention relates to a product obtained by the method according to this invention. The final product may for example be used for the outer skin of aircraft fuselages.
  • The invention in another aspect provides an apparatus for heat treating an aluminium alloy member comprising: a) a solution heat treatment furnace, b) a quenching station, c) a heating plate for reheating the member in a pre-ageing heat treatment step by coupling a main surface of the member to a main surface of the heating plate. This apparatus has the advantage that it does not require a second furnace for the pre-ageing heat treatment.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The above-mentioned and further features and advantages of the heat treatment method according to the invention will become apparent from the following detailed description of preferred embodiments, with reference to the appended drawings, in which:
  • FIG. 1 is a schematic representation of a heat treatment facility according to the prior art;
  • FIG. 2 is a schematic representation of a heat treatment facility using a method according to a first embodiment of the invention;
  • FIG. 3 is a temperature versus time graph for the method according to the first embodiment;
  • FIG. 4 is a cross sectional view of an arrangement of aluminium alloy member and heating plate according to the first embodiment;
  • FIG. 5 is a cross sectional view of an arrangement of two members and the heating plate according to a second embodiment;
  • FIG. 6 is a schematic representation of a heat treatment facility using a method according to a third embodiment of the invention
  • FIG. 7 is a cross sectional view of member/heating plate arrangement according to a further embodiment.
  • DETAILED DESCRIPTION OF THE DRAWINGS
  • FIG. 1 shows a state of the art facility for heat treating an aluminium alloy member 1. The member 1 coming from the rolling mill is solution heat treated in a continuous horizontal furnace 4. The member 1 is conveyed through the furnace on rollers 6. After solution heat treatment, the member 1 is quenched by means of nozzles 8 a, 8 b, which spray quenching water onto be upper and lower surfaces of the member. In order to reheat the member 1 for the pre-ageing heat treatment, a further horizontal furnace 10 is provided at the end of the line. Hence, the prior art method requires two furnaces. The pre-ageing furnace 10 must be specially equipped with forced hot air circulation to ensure rapid reheating of the member 1.
  • A facility implementing the method according to the first embodiment of the invention is shown in FIG. 2. The plate 1 coming from the mill is again heat treated in a horizontal furnace 4. However, it is disposed on top of a heating plate 12 during the treatment. After the solution heat treatment, the member 1 remains on the heating plate while undergoing quenching. Hence, only the upper nozzles 8 a are used to quench member 1. The member/plate arrangement is then further conveyed on rollers 6. Since plate 12 is as thick as or thicker than member 1 and made of a material of high heat capacity and good heat conductivity, plate 12 will reheat the member 1 immediately after quenching has stopped. The heating rate and the maximum temperature reached by the member will depend on the thickness and composition of the heating plate 12 in relation to the thickness and composition of the member 1. Preferably, the heating plate is about 40 mm thick, i.e. thicker than the member 1, and is preferably made of an aluminium alloy of the AA5xxx-series or AA3xxx-series.
  • The temperature profile experience by the member 1 is shown in FIG. 3. During the solution heat treatment, the member 1 is heated to a first temperature T1, which is between 450° C. and 580° C., and typically about 530° C. The metal is held at this temperature for some time as known in the art. During quenching, the metal is rapidly cooled down to a temperature of 100° C. or less, preferably to room temperature RT. By subsequently placing the member on top of heating plate 12 as shown in FIG. 2, the member will immediately be reheated to a pre-ageing temperature T2 in the range of 100° C. to 250° C., preferably in the range of 150 to 250° C. The member will reach T2 within a few minutes and will preferably be held at this temperature for a time required to achieve the desired pre-ageing effect, and the holding time would typically be in the range of up the 30 minutes, preferably 10 to 20 minutes. The selected pre-ageing temperature and holding time will be dependent on the alloy composition of the aluminium alloy member. The pre-ageing treatment is finalised by taking off the aluminium alloy member from the heating plate. The member is then cooled down to ambient temperature by means of water cooling, forced air or left on for example a roller table to cool down by free air convention. The cooling rate after the pre-ageing treatment has been found not to be very critical.
  • Most preferably, reheating to achieve the pre-ageing effect will begin within one or two minutes, preferably within 0 to 20 seconds, after quenching from solution heat treatment. The heating rate is preferably in the range of 10 to 50° C./min., so that the final pre-ageing temperature will be reached within 1 to 10 minutes, preferably 5 minutes.
  • FIG. 4 shows an enlarged cross sectional view of the member/plate arrangement. Between member and plate is disposed a protective layer 14 to space the member 1 and the plate 12 from each other, and to provide a heat isolating layer between the member 1 and the plate 12. Preferably, the protective layer 14 is about 2 mm thick and made of a heat isolating fabric such as glass fabric, glass wool, mineral wool or polymer fabric. However, any other material or any other suitable type of spacer may be used as well. Although not shown in FIG. 5 to 7, a protective layer may be present in each case between each member 1 and each heating plate 12.
  • According to a second embodiment, one heating plate 12 will be sandwiched between two aluminium alloy members 1, 1′ as shown in FIG. 5. The arrangement according to FIG. 5 allows the pre-ageing treatment of two members 1, 1′ simultaneously. The heating plate 12 must be thick enough to store sufficient heat for re-heating both members to achieve the required pre-ageing treatment.
  • These first two embodiments are suitable for continuous heat treatment, in which the heating plate(s) and the aluminium alloy member(s) are held adjacent to each other during all steps of solution heat treatment, quenching and pre-ageing.
  • However, it may be advantageous in some applications to heat up the heating plate 12 before the aluminium alloy member 1. This arrangement is shown in FIG. 6. Here, the plate 12 will be heated before the solution heat treatment of member 1 in the horizontal furnace 4 and then placed aside. After quenching, the member 1 will be lifted on top of the heating plate 12. This embodiment has the advantage that the plate 12 may have cooled down to the lower pre-ageing temperature in the range of 100 to 250° C. before receiving the member 1. Alternatively, the member 1 may be fed through the solution heat treatment furnace before the heating plate 12. The embodiment shown in FIG. 6 also allows to use a self-heating plate 12 provided e.g. with electrical coils, which need not be heated up in a furnace.
  • In another embodiment shown in FIG. 7, two heating plates 12, 12′ will be heated prior to the pre-ageing step, and one heating plate 12′ will be placed on top of member 1. This will straighten the member 1, so that further stretch forming may not be necessary.
  • After the member has cooled down to ambient temperature the member will undergo a further ageing treatment to produce an age-hardened material with the desired set of properties for its application.
  • Having now fully described the invention, it will be apparent to one of ordinary skill in the art that many changes and modifications can be made without departing from the spirit or scope of the invention as hereon described.

Claims (44)

1. A method of heat treating an aluminium alloy member having a main surface, comprising the steps of:
a) subjecting the member to a solution heat treatment,
b) quenching the member,
c) reheating the quenched member in a pre-ageing heat treatment step, and
wherein the pre-ageing heat treatment comprises coupling the main surface of the member to a main surface of a heating plate.
2. The method according to claim 1, wherein the aluminium alloy member and the heating plate are held substantially horizontally, one on top of the other, during the pre-ageing heat treatment.
3. The method according to claim 1, wherein the aluminium alloy member and the heating plate are coupled to each other during all of steps (a) to (c).
4. The method according to claim 1, wherein the heating plate is electrically heated before and/or during the pre-ageing step.
5. The method according to claim 1, wherein the heating plate is heated before the pre-ageing step by being placed in a furnace used for the solution heat treatment.
6. The method according to claim 1, wherein the aluminium alloy member is lifted onto the heating plate after the quenching step.
7. The method according to claim 1, wherein the aluminium alloy member and the heating plate are coupled to each other by placing a protective layer between the aluminium alloy member and the heating plate.
8. The method according to claim 7, wherein the protective layer is made from an isolating material selected from the group comprising glass fabric, ceramics, glass wool, mineral wool, and polymer fabric.
9. The method according to claim 7, wherein the protective layer has a thickness up to 5 mm.
10. The method according to claim 1, wherein a second aluminium alloy member is coupled with one of its main surfaces close to a second main surface of the heating plate during the pre-ageing step.
11. The method according to claim 1, wherein the aluminium alloy member is held sandwiched between two heating plates during the pre-ageing step.
12. The method as claimed in one of the preceding claims, wherein the heating plate is at least as thick as the aluminium alloy member.
13. The method according to claim 1, wherein the aluminium alloy member is a rolled product.
14. The method according to claim 1, wherein the aluminium alloy member is a rolled product having a thickness of at most 15 mm.
15. The method according to claim 1, wherein the aluminium alloy member is a rolled product having a thickness of at most 6 mm.
16. The method according to claim 1, wherein the aluminium alloy member is a rolled product having a thickness in the range of 1.5 to 6 mm.
17. The method according to claim 1, wherein the aluminium alloy member is composed of a heat-treatable aluminium alloy of the AA2xxx, AA6xxx or AA7xxx series.
18. The method according to claim 1, wherein the aluminium alloy member is composed of a heat-treatable aluminium alloy of the AA6xxx-series.
19. The method according to claim 1, wherein the aluminium alloy member is composed of a heat-treatable aluminium alloy selected from the group consisting of AA2024, M2524, AA2219, AA6013, M6056, M6011, AA6016, AA7074, AA7075, AA7055, and AA7050.
20. The method according to claim 1, wherein the aluminium alloy member is composed of a heat-treatable aluminium alloy selected from the group consisting of AA6013, M6056, AA6011, and AA6016.
21. The method according to claim 1, wherein the aluminium alloy member is for outer skin of an aircraft fuselage.
22. The method according to claim 1, wherein the heating plate has a larger heat capacity and a higher melting point relative to the aluminium alloy member.
23. The method according to claim 1, wherein the heating plate is made from an AA5xxx-series aluminium alloy.
24. The method according to claim 1, wherein the heating plate is made from an AA3xxx-series aluminium alloy.
25. The method according to claim 1, wherein the heating plate is made from steel.
26. The method according to claim 1, wherein during step b) the member is quenched to a temperature of 100° C. or less.
27. The method according to claim 1, wherein step c) starts within 2 minutes after quenching from solution heat treatment.
28. The method according to claim 1, wherein step c) starts within 20 seconds after quenching from solution heat treatment.
29. The method according to claim 1, wherein the maximum temperature of the pre-ageing heat treatment is reached within 1 to 10 minutes or less after quenching.
30. The method according to claim 1, wherein the pre-ageing treatment is carried out at a temperature in a range of 100 to 250° C.
31. The method according to claim 1, wherein the pre-ageing treatment is carried out at a temperature in a range of 150 to 250° C.
32. The method according to claim 1, wherein during the pre-ageing heat treatment step c) the aluminium alloy member is held at a pre-ageing temperature for a holding time of at most 30 minutes.
33. The method according to claim 1, further comprising the step of artificial ageing to a final temper of the aluminium alloy member which has been subjected to the pre-ageing heat treatment step (c).
34. The method according to claim 1, further comprising the step of artificial ageing to a final temper of the aluminium alloy member which has been subjected to the pre-ageing heat treatment step c), and wherein the final temper is selected from the group consisting of T6, T79, T78, T77, T74, T73, and T8.
35. The method according to claim 1, further comprising a step selected from the group consisting of stretching, compressing, and levelling, carried out after the pre-ageing heat treatment step.
36. The method according to claim 1, further comprising a step selected from the group consisting of stretching, compressing, and levelling, carried out after the pre-ageing heat treatment step and prior to artificial ageing to a final temper of the aluminium alloy member.
37. The method according to claim 1, further comprising a stretching operation by not more than 8%, said stretching operation being carried out after the pre-ageing heat treatment step.
38. The method according to claim 1, further comprising a stretching operation in a range of 1 to 5%, said stretching operation being carried out after the pre-ageing heat treatment step.
39. The method according to claim 1, further comprising a step of cold rolling carried out after the pre-ageing heat treatment step and prior to artificial ageing to a final temper of the aluminium alloy member.
40. The method according to claim 1, further comprising a step of cold rolling with a cold rolling reduction in a range of up to 20% carried out after the pre-ageing heat treatment step and prior to artificial ageing to a final temper of the aluminium alloy member.
41. A rolled aluminium alloy product produced using the heat treatment method according to claim 1.
42. A heating plate for reheating an aluminium alloy member in a pre-ageing heat treatment step by holding a main surface of the member close to a main surface of the heating plate, the heating plate having a thickness in the range of 20 mm to 50 mm.
43. A heating plate for reheating an aluminium alloy member in a pre-ageing heat treatment step by holding a main surface of the member close to a main surface of the heating plate, the heating plate having a thickness in the range of 20 mm to 50 mm, and comprising means for heating up the heating plate.
44. Apparatus for heat treating an aluminium alloy member according to the method of claim 1, comprising
a) a solution heat treatment furnace,
b) a quenching station,
c) a heating plate for reheating the member in a pre-ageing heat treatment step by holding a main surface of the member close to a main surface of the heating plate.
US11/239,477 2004-10-05 2005-09-30 Method of heat treating an aluminium alloy member and apparatus therefor Expired - Fee Related US7491278B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US11/239,477 US7491278B2 (en) 2004-10-05 2005-09-30 Method of heat treating an aluminium alloy member and apparatus therefor

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
EP04077719.5 2004-10-05
EP04077719 2004-10-05
US61622804P 2004-10-07 2004-10-07
US11/239,477 US7491278B2 (en) 2004-10-05 2005-09-30 Method of heat treating an aluminium alloy member and apparatus therefor

Publications (2)

Publication Number Publication Date
US20060070689A1 true US20060070689A1 (en) 2006-04-06
US7491278B2 US7491278B2 (en) 2009-02-17

Family

ID=36124369

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/239,477 Expired - Fee Related US7491278B2 (en) 2004-10-05 2005-09-30 Method of heat treating an aluminium alloy member and apparatus therefor

Country Status (1)

Country Link
US (1) US7491278B2 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090301617A1 (en) * 2008-06-10 2009-12-10 Gm Global Technology Operations, Inc. Sequential aging of aluminum silicon casting alloys
CN101407853B (en) * 2007-12-20 2010-08-11 北京有色金属研究总院 Quenching apparatus for detecting hardenability of aluminum alloy ultra-thick plate
US20130216790A1 (en) * 2010-11-05 2013-08-22 Aleris Aluminum Duffel Bvba Method of manufacturing a structural automotive part made from a rolled al-zn alloy
US20130334091A1 (en) * 2012-06-15 2013-12-19 Alcoa Inc. Aluminum alloys and methods for producing the same
WO2018064228A1 (en) * 2016-09-27 2018-04-05 Novelis Inc. Compact continuous annealing solution heat treatment
CN112427557A (en) * 2020-11-12 2021-03-02 中国航空制造技术研究院 Forming and shape-preserving heat treatment method for aluminum-based alloy complex-structure thin-wall component
EP3467138B1 (en) 2017-10-04 2021-11-24 Automation, Press and Tooling, A.P. & T AB Method for forming aluminum alloy blank
US11578921B2 (en) 2018-01-16 2023-02-14 Ebner Industrieofenbau Gmbh Continuous furnace for aluminum strips
US11785678B2 (en) 2016-09-27 2023-10-10 Novelis Inc. Rotating magnet heat induction

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9187800B2 (en) 2013-02-15 2015-11-17 Ford Motor Company Process control for post-form heat treating parts for an assembly operation
US8826712B1 (en) 2013-03-15 2014-09-09 Ford Global Technologies, Llc Pressure sequence process for hydro-forming an extruded structural tube
US9567660B2 (en) 2013-06-27 2017-02-14 Ford Global Technologies, Llc Method and system for using an irreversible thermo-chromatic indicator for quality assurance of a part subjected to heat treating
US20150315666A1 (en) 2014-04-30 2015-11-05 Ford Global Technologies, Llc Induction annealing as a method for expanded hydroformed tube formability

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3135633A (en) * 1959-09-08 1964-06-02 Duralumin Heat treatment process improving the mechanical properties of aluminiummagnesium-silicon alloys
US4294625A (en) * 1978-12-29 1981-10-13 The Boeing Company Aluminum alloy products and methods
US5258081A (en) * 1989-10-12 1993-11-02 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Auxiliary heat treatment for aluminium-lithium alloys
US5662750A (en) * 1995-05-30 1997-09-02 Kaiser Aluminum & Chemical Corporation Method of manufacturing aluminum articles having improved bake hardenability
US5718780A (en) * 1995-12-18 1998-02-17 Reynolds Metals Company Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom
US5728241A (en) * 1993-07-28 1998-03-17 Alcan International Limited Heat treatment process for aluminum alloy sheet
US6406571B1 (en) * 1999-05-14 2002-06-18 Alcan International Limited Heat treatment of formed aluminum alloy products
US20020174920A1 (en) * 2000-06-01 2002-11-28 Gupta Alok Kumar Heat treatment of formed aluminum alloy products
US20030015261A1 (en) * 2001-05-03 2003-01-23 Bull Michael Jackson Process for preparing an aluminum alloy sheet with improved bendability and aluminum alloy sheet produced therefrom

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB292690A (en) 1927-03-25 1928-06-25 Henry Winder Brownsdon Improvements in and relating to the annealing of metal
DE908735C (en) 1939-05-12 1954-04-08 Siemens Ag Process and device for annealing metallic hollow bodies with thin walls and thick bases
GB1258147A (en) * 1969-11-25 1971-12-22
PL139785B1 (en) 1984-01-03 1987-02-28 Gdanskie Zaklady Rafineryjne Method of obtaining a catalyst for hydrorefining of lubricating oils in particular for refining processes being carried out under mild conditions
DE69107392T2 (en) 1990-10-09 1995-06-08 Sumitomo Light Metal Ind Process for producing a material from an aluminum alloy with excellent press formability and baking hardenability.
FR2713664B1 (en) 1993-11-17 1996-05-24 Pechiney Rhenalu Al-Si-Mg alloy with improved ductility and stampability and process for obtaining it.
NL1002861C2 (en) * 1996-04-15 1997-10-17 Hoogovens Aluminium Nv Method for manufacturing a highly deformable aluminum sheet.
DE19907497C2 (en) 1999-02-22 2003-05-28 Steag Hamatech Ag Device and method for heat treatment of substrates
DE10043562C2 (en) 1999-09-16 2003-09-18 Honsel Profilprodukte Gmbh Process for the heat treatment of extruded profiles

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3135633A (en) * 1959-09-08 1964-06-02 Duralumin Heat treatment process improving the mechanical properties of aluminiummagnesium-silicon alloys
US4294625A (en) * 1978-12-29 1981-10-13 The Boeing Company Aluminum alloy products and methods
US5258081A (en) * 1989-10-12 1993-11-02 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Auxiliary heat treatment for aluminium-lithium alloys
US5728241A (en) * 1993-07-28 1998-03-17 Alcan International Limited Heat treatment process for aluminum alloy sheet
USRE36692E (en) * 1993-07-28 2000-05-16 Alcan International Limited Heat treatment process for aluminum alloy sheet
US5662750A (en) * 1995-05-30 1997-09-02 Kaiser Aluminum & Chemical Corporation Method of manufacturing aluminum articles having improved bake hardenability
US5718780A (en) * 1995-12-18 1998-02-17 Reynolds Metals Company Process and apparatus to enhance the paintbake response and aging stability of aluminum sheet materials and product therefrom
US6406571B1 (en) * 1999-05-14 2002-06-18 Alcan International Limited Heat treatment of formed aluminum alloy products
US20020174920A1 (en) * 2000-06-01 2002-11-28 Gupta Alok Kumar Heat treatment of formed aluminum alloy products
US20030015261A1 (en) * 2001-05-03 2003-01-23 Bull Michael Jackson Process for preparing an aluminum alloy sheet with improved bendability and aluminum alloy sheet produced therefrom

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101407853B (en) * 2007-12-20 2010-08-11 北京有色金属研究总院 Quenching apparatus for detecting hardenability of aluminum alloy ultra-thick plate
US20090301617A1 (en) * 2008-06-10 2009-12-10 Gm Global Technology Operations, Inc. Sequential aging of aluminum silicon casting alloys
US8728258B2 (en) * 2008-06-10 2014-05-20 GM Global Technology Operations LLC Sequential aging of aluminum silicon casting alloys
US20130216790A1 (en) * 2010-11-05 2013-08-22 Aleris Aluminum Duffel Bvba Method of manufacturing a structural automotive part made from a rolled al-zn alloy
US9493867B2 (en) * 2010-11-05 2016-11-15 Aleris Aluminum Duffel Bvba Method of manufacturing a structural automotive part made from a rolled Al—Zn alloy
US20130334091A1 (en) * 2012-06-15 2013-12-19 Alcoa Inc. Aluminum alloys and methods for producing the same
US9856552B2 (en) * 2012-06-15 2018-01-02 Arconic Inc. Aluminum alloys and methods for producing the same
RU2721970C1 (en) * 2016-09-27 2020-05-25 Новелис Инк. Heating with magnetic metal suspension with surface quality control
US11072843B2 (en) 2016-09-27 2021-07-27 Novelis Inc. Systems and methods for non-contact tensioning of a metal strip
AU2017336561B2 (en) * 2016-09-27 2019-12-12 Novelis Inc. Compact continuous annealing solution heat treatment
US10508328B2 (en) 2016-09-27 2019-12-17 Novelis Inc. Rapid heating of sheet metal blanks for stamping
RU2709494C1 (en) * 2016-09-27 2019-12-18 Новелис Инк. Compact homogenization line by continuous annealing
WO2018064228A1 (en) * 2016-09-27 2018-04-05 Novelis Inc. Compact continuous annealing solution heat treatment
US10837090B2 (en) 2016-09-27 2020-11-17 Novelis Inc. Magnetic levitation heating of metal with controlled surface quality
US10844467B2 (en) 2016-09-27 2020-11-24 Novelis Inc. Compact continuous annealing solution heat treatment
US11821066B2 (en) 2016-09-27 2023-11-21 Novelis Inc. Systems and methods for non-contact tensioning of a metal strip
US10370749B2 (en) 2016-09-27 2019-08-06 Novelis Inc. Systems and methods for threading a hot coil on a mill
US11785678B2 (en) 2016-09-27 2023-10-10 Novelis Inc. Rotating magnet heat induction
US11242586B2 (en) 2016-09-27 2022-02-08 Novelis Inc. Systems and methods for threading a hot coil on a mill
US11377721B2 (en) 2016-09-27 2022-07-05 Novelis Inc. Systems and methods for threading a hot coil on a mill
US11479837B2 (en) * 2016-09-27 2022-10-25 Novelis Inc. Pre-ageing systems and methods using magnetic heating
US11499213B2 (en) 2016-09-27 2022-11-15 Novelis Inc. Systems and methods for threading a hot coil on a mill
US20230002876A1 (en) * 2016-09-27 2023-01-05 Novelis Inc. Pre-ageing systems and methods using magnetic heating
EP3467138B1 (en) 2017-10-04 2021-11-24 Automation, Press and Tooling, A.P. & T AB Method for forming aluminum alloy blank
US11578921B2 (en) 2018-01-16 2023-02-14 Ebner Industrieofenbau Gmbh Continuous furnace for aluminum strips
CN112427557A (en) * 2020-11-12 2021-03-02 中国航空制造技术研究院 Forming and shape-preserving heat treatment method for aluminum-based alloy complex-structure thin-wall component

Also Published As

Publication number Publication date
US7491278B2 (en) 2009-02-17

Similar Documents

Publication Publication Date Title
US7491278B2 (en) Method of heat treating an aluminium alloy member and apparatus therefor
EP1797210A1 (en) Method of heat treating an aluminium alloy member and apparatus therefor
US11806779B2 (en) Systems and methods for making thick gauge aluminum alloy articles
CN106591650B (en) A method of improving aluminium lithium alloy anti-stress corrosion performance
EP1831415B1 (en) Method for producing a high strength, high toughness al-zn alloy product
US20070187007A1 (en) Aluminum-zinc-magnesium-copper alloy extrusion
US20080299000A1 (en) Aluminum-zinc-copper-magnesium-silver alloy wrought product
JP2022512876A (en) 7XXX series aluminum alloy products
JP2008516079A5 (en)
CN100577848C (en) Method for producing a high damage tolerant aluminium alloy
CN112262223B (en) Method of manufacturing 7 xxx-series aluminum alloy sheet products having improved fatigue failure resistance
JP2007510061A5 (en)
US5785777A (en) Method of making an AA7000 series aluminum wrought product having a modified solution heat treating process for improved exfoliation corrosion resistance
CA2446393A1 (en) Method of quenching alloy sheet to minimize distortion
US6569271B2 (en) Aluminum alloys and methods of making the same
US9314826B2 (en) Method for the manufacture of an aluminium alloy plate product having low levels of residual stress
CN107502796B (en) A kind of Sc-Zr-Yb composite strengthening Al-Zn-Mg alloy and preparation method thereof
EP1244819B1 (en) Method of quenching an alloy sheet to minimize distortion
US20050098245A1 (en) Method of manufacturing near-net shape alloy product
CN116043153B (en) Method for improving strength and plasticity of metastable beta titanium alloy dual-performance structural member
CN116940699A (en) High strength 5XXX aluminum alloy variants and methods for making the same

Legal Events

Date Code Title Description
AS Assignment

Owner name: CORUS ALUMINIUM WALZPRODUKTE GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:KROPFL, INGO GUNTHER;REEL/FRAME:017374/0524

Effective date: 20051027

AS Assignment

Owner name: ALERIS ALUMINUM KOBLENZ GMBH, GERMANY

Free format text: CHANGE OF NAME;ASSIGNOR:CORUS ALUMINIUM WALZPRODUKTE GMBH;REEL/FRAME:021820/0094

Effective date: 20061222

STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

FPAY Fee payment

Year of fee payment: 8

FEPP Fee payment procedure

Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

LAPS Lapse for failure to pay maintenance fees

Free format text: PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20210217